Analysis of Flutter in Compressible Flow of a Panel on Many Supports
Author:
Affiliation:
1. Langley Aeronautical Laboratory, NACA,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3089
Reference9 articles.
1. Miles, J. W., Dynamic Chordwise Stability at Supersonic Speeds, North American Aviation Report AL-1140, 1950.
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